@inproceedings{oai:jaxa.repo.nii.ac.jp:00006327,
 author = {川崎, 崇 and 細田, 聡史 and Kim, Jeongho and Cho, Mengu and Kawasaki, Takashi and Hosoda, Satoshi and Kim, Jeongho and Cho, Mengu},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: 9th Spacecraft Charging Technology Conference},
 month = {Aug},
 note = {The purpose of this research is to investigate the influence of coverglass on arcing phenomena on GEO satellite solar array. Experiments were performed by using a large solar array coupon (400 x 400 mm). The Coupon has 50 Si cells. We measured surface potential on the solar array coupon immediately after arc inception. Extent of neutralization differed for each arc. Less charge was neutralized as the distance from arc position increases. At the worst case, 53 percent charge was neutralized at 325 mm in this experiment. Arc plasma propagation velocity was of the order of 10(exp 4) m/s but differed widely for each arc., 資料番号: AA0049206012, レポート番号: JAXA-SP-05-001E},
 pages = {95--103},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ESD test of large solar array coupon in GEO plasma environment},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}